de Havilland Canada DHC-2 Beaver vs. Sukhoi Su-57

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de Havilland Canada DHC-2 Beaver versus Sukhoi Su-57
13.56 m 44 ft 6 in length 20.1 m 65 ft 11 in
5 m 16 ft 5 in height 3.8 m 12 ft 6 in
16.56 m 54 ft 4 in wingspan 14.1 m 46 ft 3 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 2 (Izdeliye 117 or AL-41F1 augmented turbofans)
Approximately 3,100 hp (2,312 kW) each thrust per engine 107.9 kN dry and 166.8 kN after burning
Approximately 6,200 hp (4,624 kW) total total thrust 215.8 kN dry and 333.6 kN after burning
24,200 lb 10,977 kg MTOW 35,000 kg 77,200 lb
2,535 km 1,369 nm range 3,500 km 1,890 nm
228 mph 367 km/h cruise speed Mach 2 2470 km/h
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.